CESSNA
MODEL 162
GARMIN G300
SAMPLE PROBLEM
LANDING
A procedure similar to takeoff should be used for estimating the landing
distance at the destination airport. Figure 5-4 presents landing distance
information for the short field technique. The distances corresponding
to 2000 feet and 30°C are as follows:
Ground roll
Total distance to clear a 50-foot obstacle
A correction for the effect of wind may be made based on information
presented in the note section of the landing chart, using the same
procedure as outlined for takeoff.
DEMONSTRATED OPERATING TEMPERATURE
Satisfactory engine cooling has been demonstrated for this airplane
with an outside air temperature 23°C above standard. This is not to be
considered as an operating limitation. Reference should be made to
Section 2 for engine operating limitations.
162PHUS-01
(Continued)
SECTION 5
PERFORMANCE
760 Feet
1485 Feet
U.S.
5-9